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  KEYWORD

Application of machine learning techniques to aerodynamic optimization of missile configurations

azienda Thesis in external company    


keywords MACHINE LEARNING, NUMERICAL MODELS AND METHODS, OPTIMIZATION, SCIENTIFIC COMPUTING

Reference persons STEFANO BERRONE

External reference persons Referente aziendale

Research Groups Analisi numerica e calcolo scientifico

Thesis type TESI CON STAGE AZIENDALE

Description The purpose of this Master's thesis proposal is to evaluate the applicability of techniques related to artificial intelligence, and in particular of machine learning applied to the field of aerodynamic shape optimization in the missile field.

Required skills Matlab, Numerical Methods, Fluid Dynamics and Aeordynamic, Basic notions in Machine Learning


Deadline 02/10/2020      PROPONI LA TUA CANDIDATURA




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